MALE UAV LONGITUDINAL STABILITY DETERMINATION USING WIND TUNNEL DATA
Muhammad Ilham Adhynugraha(1), Fadli Cahya Megawanto(2), Siti Vivi Octaviany(3), Dewi Habsari Budiarti(4*), Jemie Muliadi(5), Osen Fili Nami(6), Singgih Satrio Wibowo(7)
(1) National Research and Innovation Agency
(2) National Research and Innovation Agency
(3) National Research and Innovation Agency
(4) National Research and Innovation Agency
(5) National Research and Innovation Agency
(6) National Research and Innovation Agency
(7) Politeknik Negeri Bandung
(*) Corresponding Author
Abstract
Unmanned aerial systems have been increasing in demand for a wide range of operations, including the rapid growth of advanced navigation and communication. One of the most important things in designing an Unmanned Aerial System (UAS) is to ensure the system's stability, such as the UAS itself. This study was conducted on an in-house medium altitude long endurance (MALE) UAS aircraft. It is focused on analyzing the longitudinal stability of MALE UAS. A mathematical approach was used to analyze the longitudinal stability. A series of wind tunnel tests using a scaled model of the MALE UAS is done to produce several sets of data containing longitudinal stability derivatives for various configurations. A few sets of data are chosen to obtain the stability derivatives needed. These stability derivatives are utilized to determine the longitudinal motion characteristic of the aircraft. The analysis of certain derivatives and the phugoid and short-period mode shows that the aircraft is statically and dynamically stable in longitudinal motion. The results indicated that a weight change prompted an altercation in the natural frequency of the short-period mode. The response also showed that reaching a new equilibrium state takes a rather long period after an arbitrary perturbation is initiated. The time required to subdue oscillation in axial and average velocities is more than 100 seconds. The stability in the pitch rate is reached in around 65 seconds. The time to reach stability in pitch angle response is around 65 seconds.
Keywords
Full Text:
PDFReferences
Colomina, I. and Molina, P. (2014). Unmanned aerial systems for photogrammetry and remote sensing: A review. ISPRS Journal of Photogrammetry and Remote Sensing. Remote Sens. 92, 79–97. https://doi.org/10.1016/j.isprsjprs.2014.02.013
Cook, M.V. (2007). Flight Dynamics Principles. Book: Flight Dynamics Principles. https://doi.org/10.1016/B978-0-7506-6927-6.X5000-4
Gertler, J. (2012). U.S. unmanned aerial systems. Unmanned Aerial Systems (UAS). Drones Blimps 1–50.
Henry, J., Blondeau, J., and Pines, D. (2005). Stability Analysis for UAVs with a Variable Aspect Ratio Wing. 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. https://doi.org/10.2514/6.2005-2044
Iqbal, L., Crossley, W., Weisshaar, T., Sullivan, J. (2008). Higher Level Design Methods Applied to the Conceptual Design of an MALE UAV. 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. https://doi.org/10.2514/6.2008-5908
Iqbal, L., Sullivan, J. (2009). Comprehensive Aircraft Preliminary Design Methodology Applied to the Design of MALE UAV, 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. https://doi.org/10.2514/6.2009-431
Li, X. and Savkin, A. (2021). Networked Unmanned Aerial Vehicles for Surveillance and Monitoring: A Survey. Futur. Internet 13, 174. https://doi.org/10.3390/fi13070174
Adeleke, O.A., Abbe, G.E., Jemitola, P.O. and Thomas, S. (2022). Design of the wing of a medium altitude long endurance UAV. International Journal of Engineering and Manufacturing (IJEM), 12(1), pp.37-47. https://doi.org/10.5815/ijem.2022.01.04
O’Donnell, R. and Mohseni, K. (2018). Aerodynamic parameter estimation from wind tunnel testing of a small UAS. AIAA Atmospheric Flight Mechanics Conference. https://doi.org/10.2514/6.2018-0294
Purwadi, P. (2019). Peran Laboratorium Pengujian Aerodinamika Pada Percepatan Kemandirian Bangsa. Prosiding SENIATI, 5(1), pp.370-376. https://doi.org/10.36040/seniati.v5i1.465
Sakya, A.E., Wiriadidjaja, S. and Adibroto, A. (1998). Commemorating Ten Years Operation Of The Indonesian Low Speed Tunnel (ILST). 21st Congress of International Council of the Aeronautical Sciences, Melbourne, Australia, 13-18 September, 1998
Paper ICAS-98-3.11.3
Hasim, F., Rusyadi, R., Surya, W.I., Asrar, W., Omar, A.A., Mohamed Ali, J.S. and Kafafy, R., (2008). December. The IIUM low speed wind tunnel. In Proceedings of the 2nd Engineering Conference on Sustainable Engineering Infrastructures Development & Management (EnCon2008).
Purwadi, P., Hidayat, A.R., Hariz, I., Satriya, I.A.A., Kuswandi, K., Triwulandari, R. and Pinindriya, S.T. (2023). December. Designing of hinge moment balance for hinge rudder performance measurement in Indonesian low speed tunnel (ILST). In AIP Conference Proceedings (Vol. 2941, No. 1). AIP Publishing. https://doi.org/10.1063/5.0181422
Soemaryanto, A.R., Herdiana, D., Wahyudi, W., Triwulandari, R. and Aziz, M.N. (2023). December. Parametric study of extended horizontal tailplane of commuter aircraft using wind tunnel testing. In AIP Conference Proceedings (Vol. 2941, No. 1). AIP Publishing. https://doi.org/ 10.1063/5.0181442
Adhynugraha, M.I., Budiarti, D.H., Muliadi, J., Nami, O.F., Octaviany, S.V. and Megawanto, F.C. (2023). December. Effect of tail and ruddervator on aerodynamics of UAV through wind tunnel study. In AIP Conference Proceedings (Vol. 2941, No. 1). AIP Publishing. https://doi.org/10.1063/5.0181637
Panagiotou, P, Fotiadis-Karras, S., and Yakinthos, K. (2018). Conceptual design of a Blended Wing Body MALE UAV. Aerospace Science and Technology. 73, 32–47. https://doi.org/https://doi.org/10.1016/j.ast.2017.11.032
Panagiotou, Pericles, Giannakis, E., Savaidis, G., and Yakinthos, K. (2018). Aerodynamic and structural design for the development of a MALE UAV. Aircraft Engineering and Aerospace Technology. 90. https://doi.org/10.1108/AEAT-01-2017-0031
Panagiotou, P., Kaparos, P., Salpingidou, C., and Yakinthos, K. (2016). Aerodynamic design of a MALE UAV. Aerospace Science and Technology. 50. https://doi.org/10.1016/j.ast.2015.12.033
Stodola, P., Drozd, J., Mazal, J., Hodicky, J., and Prochazka, D. (2019). Cooperative Unmanned Aerial System Reconnaissance in a Complex Urban Environment and Uneven Terrain. Sensors 19, 3754. https://doi.org/10.3390/s19173754
Taylor, D. (2010). Marine: Demand “beginning to boil”: ONR Meets With Industry For Long-Term Cargo UAS Program In Mid-2010s. Insid. Navy 23, 1–12.
Wienke, F., Raffel, M., and Dillmann, A. (2021). Wind Tunnel Testing of Otto Lilienthal’s Production Aircraft from 1893. American Institute of Aeronautics and Astronautics (AIAA) Journal. 59, 1342–1351.
DOI: https://doi.org/10.22146/teknosains.89420
Article Metrics
Abstract views : 143 | views : 138Refbacks
- There are currently no refbacks.
Copyright (c) 2024 Muhammad Ilham Adhynugraha, et al.
This work is licensed under a Creative Commons Attribution-ShareAlike 4.0 International License.
Copyright © 2024 Jurnal Teknosains Submit an Article Tracking Your Submission
Editorial Policies Publishing System Copyright Notice Site Map Journal History Visitor Statistics Abstracting & Indexing